17
17
17
foD protection
Inertial Separator
The nacelle inlet of many aircraft models includes an inertial separator
provided by the aircraft manufacturer to prevent heavy particles from
entering the engine inlet. Most installations incorporate two moveable
vanes, one upstream of the engine inlet and the other blocking the bypass
duct. For bypass operation, the inlet vane is lowered and the bypass
duct vane is opened permitting maximum separating efficiency. In some
installations, the vanes are fixed in the bypass mode.
As shown in the sketch, air entering the engine inlet must turn sharply past
the inlet vane (shown in the lowered position). Particles heavier than air
are carried straight through, by their own inertia, into the bypass duct and
dumped overboard.
The aft radial inlet design provides many advantages such as superior
anti-icing utilizing the principle of inertial separation, low noise levels and
unequalled protection from FOD.
BYPASS (ICING)
POSITION
NORMAL
POSITION
foD protection
Inertial Separator
The nacelle inlet of many aircraft models includes an inertial separator
provided by the aircraft manufacturer to prevent heavy particles from
entering the engine inlet. Most installations incorporate two moveable
vanes, one upstream of the engine inlet and the other blocking the bypass
duct. For bypass operation, the inlet vane is lowered and the bypass
duct vane is opened permitting maximum separating efficiency. In some
installations, the vanes are fixed in the bypass mode.
As shown in the sketch, air entering the engine inlet must turn sharply past
the inlet vane (shown in the lowered position). Particles heavier than air
are carried straight through, by their own inertia, into the bypass duct and
dumped overboard.
The aft radial inlet design provides many advantages such as superior
anti-icing utilizing the principle of inertial separation, low noise levels and
unequalled protection from FOD.
BYPASS (ICING)
POSITION
NORMAL
POSITION
Summary of Contents for PT6A Turboprop
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